NUSAT-53 (JANE GOODALL), 68432
Orbit data source: Space-Track
NUSAT-53 (JANE GOODALL), 68432 is a payload satellite owned by URUGUS S.A. (AR) in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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68432 intel report (Beta)
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Identifier
Orbit
Country
AR / ARGNRelated business
Manufacturer
URUGUS S.A.
Mission
Operational spacecraft
Bus & Motor
NEWSAT V, Unknown motor
Mass
41.5 kg wet, 38.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 NUSAT-53 (JANE GOODALL)
1 68432U 26067S 26171.42849539 .00004931 00000-0 24162-3 0 9990
2 68432 97.4560 129.8799 0003376 49.0117 311.1409 15.18603480 12437Epoch: 2026-06-20T10:17Z
TLE epoch observation values (Epoch: 2026-06-20T10:17:02.001Z)
Latitude
-0.00002°
Longitude
66.97831°
Altitude
511.618 km
Speed
7.609 km/s
True Right ascension
08h 39m 31s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:06:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.355 km
Perigee altitude
504.706 km
Semi-major axis
6,885.167 km
Eccentricity
0.00034
Inclination
97.456°
RAAN
129.8799°
Arg. of periapsis
49.0117°
True anomaly
311.11176°
Mean anomaly
311.1409°
Eccentric anomaly
311.12633°
Mean motion
3.79902 °/min
Orbital period
94.76 mins
BSTAR
0.00024162
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Other satellites on launch #67 in the year 2026 (2026-03-30 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NUSAT-53 (JANE GOODALL) Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 10:16:35.842Z | 6.072° NNE | 2026-06-22 10:20:35.842Z | 244.2° WSW | 41.012° | 2026-06-22 10:23:35.842Z | 202.453° SSW |
| 5 mins | 2026-06-22 20:56:35.842Z | 135.697° SSE | 2026-06-22 20:58:35.842Z | 73.497° E | 35.258° | 2026-06-22 21:01:35.842Z | 3.699° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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